View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 47135U 26145.29697331 +.00000000 +00000-0 +73978-3 0 00008
2 47135 53.0462 262.8242 0002594 238.9819 121.0942 15.68880434 04
| Epoch (UTC): | 25 May 2026 07:07:38 |
| Eccentricity: | 0.0002594 |
| inclination: | 53.0462° |
| perigee height: | 360 km |
| apogee height: | 364 km |
| right ascension of ascending node: | 262.8242° |
| argument of perigee: | 238.9819° |
| revolutions per day: | 15.68880434 |
| mean anomaly at epoch: | 121.0942° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|